WO2019156720A1 - Dispositif de logement de rouleaux pour roulements à rouleaux coniques - Google Patents

Dispositif de logement de rouleaux pour roulements à rouleaux coniques Download PDF

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Publication number
WO2019156720A1
WO2019156720A1 PCT/US2018/055351 US2018055351W WO2019156720A1 WO 2019156720 A1 WO2019156720 A1 WO 2019156720A1 US 2018055351 W US2018055351 W US 2018055351W WO 2019156720 A1 WO2019156720 A1 WO 2019156720A1
Authority
WO
WIPO (PCT)
Prior art keywords
roller seating
ring
bearing assembly
roller
assembly
Prior art date
Application number
PCT/US2018/055351
Other languages
English (en)
Inventor
Hiroshi Marunaka
Original Assignee
The Timken Company
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by The Timken Company filed Critical The Timken Company
Priority to ES18797280T priority Critical patent/ES2934069T3/es
Priority to EP18797280.7A priority patent/EP3749871B1/fr
Priority to US16/967,326 priority patent/US20200362917A1/en
Priority to CN201880092082.3A priority patent/CN111919043B/zh
Publication of WO2019156720A1 publication Critical patent/WO2019156720A1/fr

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C35/00—Rigid support of bearing units; Housings, e.g. caps, covers
    • F16C35/04—Rigid support of bearing units; Housings, e.g. caps, covers in the case of ball or roller bearings
    • F16C35/06—Mounting or dismounting of ball or roller bearings; Fixing them onto shaft or in housing
    • F16C35/063—Fixing them on the shaft
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C43/00—Assembling bearings
    • F16C43/04—Assembling rolling-contact bearings
    • F16C43/06—Placing rolling bodies in cages or bearings
    • F16C43/065—Placing rolling bodies in cages or bearings in cages
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P15/00—Making specific metal objects by operations not covered by a single other subclass or a group in this subclass
    • B23P15/003—Making specific metal objects by operations not covered by a single other subclass or a group in this subclass bearings
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C19/00—Bearings with rolling contact, for exclusively rotary movement
    • F16C19/22—Bearings with rolling contact, for exclusively rotary movement with bearing rollers essentially of the same size in one or more circular rows, e.g. needle bearings
    • F16C19/34—Bearings with rolling contact, for exclusively rotary movement with bearing rollers essentially of the same size in one or more circular rows, e.g. needle bearings for both radial and axial load
    • F16C19/38—Bearings with rolling contact, for exclusively rotary movement with bearing rollers essentially of the same size in one or more circular rows, e.g. needle bearings for both radial and axial load with two or more rows of rollers
    • F16C19/383—Bearings with rolling contact, for exclusively rotary movement with bearing rollers essentially of the same size in one or more circular rows, e.g. needle bearings for both radial and axial load with two or more rows of rollers with tapered rollers, i.e. rollers having essentially the shape of a truncated cone
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C25/00—Bearings for exclusively rotary movement adjustable for wear or play
    • F16C25/06—Ball or roller bearings
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C41/00—Other accessories, e.g. devices integrated in the bearing not relating to the bearing function as such
    • F16C41/04—Preventing damage to bearings during storage or transport thereof or when otherwise out of use
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C43/00—Assembling bearings
    • F16C43/04—Assembling rolling-contact bearings
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C19/00—Bearings with rolling contact, for exclusively rotary movement
    • F16C19/22—Bearings with rolling contact, for exclusively rotary movement with bearing rollers essentially of the same size in one or more circular rows, e.g. needle bearings
    • F16C19/34—Bearings with rolling contact, for exclusively rotary movement with bearing rollers essentially of the same size in one or more circular rows, e.g. needle bearings for both radial and axial load
    • F16C19/38—Bearings with rolling contact, for exclusively rotary movement with bearing rollers essentially of the same size in one or more circular rows, e.g. needle bearings for both radial and axial load with two or more rows of rollers
    • F16C19/383—Bearings with rolling contact, for exclusively rotary movement with bearing rollers essentially of the same size in one or more circular rows, e.g. needle bearings for both radial and axial load with two or more rows of rollers with tapered rollers, i.e. rollers having essentially the shape of a truncated cone
    • F16C19/385—Bearings with rolling contact, for exclusively rotary movement with bearing rollers essentially of the same size in one or more circular rows, e.g. needle bearings for both radial and axial load with two or more rows of rollers with tapered rollers, i.e. rollers having essentially the shape of a truncated cone with two rows, i.e. double-row tapered roller bearings
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2226/00—Joining parts; Fastening; Assembling or mounting parts
    • F16C2226/50—Positive connections
    • F16C2226/60—Positive connections with threaded parts, e.g. bolt and nut connections
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2229/00—Setting preload
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2237/00—Repair or replacement
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2300/00—Application independent of particular apparatuses
    • F16C2300/10—Application independent of particular apparatuses related to size
    • F16C2300/14—Large applications, e.g. bearings having an inner diameter exceeding 500 mm
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2360/00—Engines or pumps
    • F16C2360/31—Wind motors
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C33/00—Parts of bearings; Special methods for making bearings or parts thereof
    • F16C33/30—Parts of ball or roller bearings
    • F16C33/46—Cages for rollers or needles
    • F16C33/4694—Single-split roller or needle cages
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C33/00—Parts of bearings; Special methods for making bearings or parts thereof
    • F16C33/30—Parts of ball or roller bearings
    • F16C33/46—Cages for rollers or needles
    • F16C33/48—Cages for rollers or needles for multiple rows of rollers or needles
    • F16C33/485—Cages for rollers or needles for multiple rows of rollers or needles with two or more juxtaposed cages joined together or interacting with each other
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C33/00—Parts of bearings; Special methods for making bearings or parts thereof
    • F16C33/30—Parts of ball or roller bearings
    • F16C33/58—Raceways; Race rings
    • F16C33/583—Details of specific parts of races
    • F16C33/585—Details of specific parts of races of raceways, e.g. ribs to guide the rollers
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C33/00—Parts of bearings; Special methods for making bearings or parts thereof
    • F16C33/30—Parts of ball or roller bearings
    • F16C33/58—Raceways; Race rings
    • F16C33/60—Raceways; Race rings divided or split, e.g. comprising two juxtaposed rings
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C35/00—Rigid support of bearing units; Housings, e.g. caps, covers
    • F16C35/04—Rigid support of bearing units; Housings, e.g. caps, covers in the case of ball or roller bearings
    • F16C35/042—Housings for rolling element bearings for rotary movement
    • F16C35/045—Housings for rolling element bearings for rotary movement with a radial flange to mount the housing
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C35/00—Rigid support of bearing units; Housings, e.g. caps, covers
    • F16C35/04—Rigid support of bearing units; Housings, e.g. caps, covers in the case of ball or roller bearings
    • F16C35/06—Mounting or dismounting of ball or roller bearings; Fixing them onto shaft or in housing
    • F16C35/067—Fixing them in a housing

Definitions

  • the present invention relates to tapered roller bearings, and more specifically to bearings used for supporting a mainshaft of a wind turbine.
  • Fig. 1 illustrates a conventional wind turbine drive train configuration 10 including a three-point mounting system 12.
  • the wind turbine drive train configuration 10 supports turbine blades 15 coupled to a nosecone 20, which in turn, is coupled to a wind turbine mainshaft 25 on three points of support.
  • a first support is an upwind pillowblock 30 that normally contains a two-row spherical roller bearing 32 and is attached to a bedplate 35.
  • Second and third supports are downwind and are two attachment points 40, 45 (e.g., torque arms) that are attached to the bedplate 35.
  • Each torque arm 40, 45 is positioned on a side of a gearbox 50.
  • FIG. 2 illustrates a four-point mounting system 55 of another conventional wind turbine drive train configuration 10’.
  • the four-point mounting system 55 supports the mainshaft 25 upwind and downwind on two pillowblocks 30.
  • Each pillowblock 30 contains a two-row spherical roller bearing 32. Combined, there are four-supporting bearing rows in a four-point mounting.
  • the invention provides an assembly tool for positioning the rolling elements of a bearing assembly during a preloading operation.
  • the assembly tool includes a roller seating actuator configured to be removably coupled to a portion of the bearing assembly during the preloading operation, and a roller seating ring movably coupled to the roller seating actuator.
  • the roller seating ring includes a distal end configured to engage an end of a rolling element of the bearing assembly.
  • a biasing member is positioned between the roller seating actuator and the roller seating ring and biases the roller searing ring away from roller seating actuator such that the distal end of the roller seating ring engages and presses the rolling element axially into engagement with a rib of a race of the bearing assembly.
  • the invention provides a method of installing and preloading a roller bearing assembly about a shaft.
  • the roller bearing assembly includes an inner ring defining thereon an inner raceway, an outer ring defining thereon an outer raceway, a rib adjacent at least one of the inner and outer raceways, a plurality of rolling elements positioned between the inner and outer raceways, a housing radially outside of the outer ring, and a clamping plate coupled with the housing via an adjustable clamping member and abutting the outer ring.
  • the method includes installing each of the inner ring, the outer ring, the plurality of rolling elements, the housing, and the clamping plate about the shaft and removably coupling an assembly tool to at least one of the housing and the clamping plate.
  • the assembly tool includes a roller seating actuator removably coupled to at least one of the housing and the clamping plate, and a roller seating ring movably coupled to the roller seating actuator.
  • the roller seating ring includes a distal end engaging respective ends of the rolling elements of the bearing assembly.
  • a biasing member is positioned between the roller seating actuator and the roller seating ring and biases the roller seating ring away from roller seating actuator such that the distal end of the roller seating ring engages and presses the rolling elements axially into engagement with the rib.
  • the method further includes preloading the bearing assembly by adjusting the adjustable clamping member while the rolling elements are pressed against the rib by the assembly tool, and removing the assembly tool from the bearing assembly after the preloading step has been completed.
  • the biasing member could be eliminated such that the roller seating actuator and the roller seating ring are axially spaced by a fixed distance.
  • the mounting of the roller seating actuator to the bearing assembly could create the desired axial force on the rollers.
  • the roller seating actuator and the roller seating ring could be integrated into a single part.
  • FIG. 1 illustrates a conventional three-point mounting arrangement for a wind turbine mainshaft.
  • FIG. 2 illustrates a conventional four-point mounting arrangement for a wind turbine mainshaft.
  • Fig. 3 is an exploded view of a split pillowblock and bearing assembly configured to rotatably support a wind turbine mainshaft.
  • Fig. 4 is a section view of the split pillowblock and bearing assembly of Fig. 3
  • Fig. 5 is a partial section view of the partially -installed split pillowblock and bearing assembly of Fig. 3 illustrating the use of a roller seating device embodying the invention during the installation process.
  • FIG. 6 is a partial perspective view of another roller seating device embodying the invention.
  • Fig. 7 is an end view of the roller seating device of Fig. 6
  • FIG. 8 is a perspective view of the roller seating ring of the roller seating device of
  • Fig. 9 is a side view of the roller seating actuator of the roller seating device of Fig. 6.
  • Fig. 10 is a partial section view illustrating the roller seating device of Fig. 6 in use during installation of the split pillowblock and bearing assembly.
  • This invention was developed originally for use with a split pillowblock bearing used for supporting a mainshaft of a wind turbine and will be described as used in that application. However, this invention can also be used in other applications benefitting from split bearings in both pillowblock and non-pillowblock applications.
  • split bearings are often used in industries such as power generation, pulp and paper, mining, cement, metals, marine and waste water. Common applications are pulverizers, crushers, fans, blowers, centrifuges, conveyors, and marine propulsion shafts.
  • Figs. 3 and 4 illustrate a split pillowblock and bearing assembly 100 coupled to the wind turbine mainshaft 25 about a bearing central axis 105 (see Fig. 3).
  • the split pillowblock and bearing assembly 100 can be installed with the aid of an assembly tool 104, 104’ (see Figs. 5-10) in the form of a roller seating device embodying the present invention.
  • the bearing assembly 100 can be a replacement to an existing spherical or other type of bearing being removed from the wind turbine, or can be an original bearing in a newly- constructed wind turbine. Referring to Fig.
  • split housing is defined by pillowblocks (i.e., a lower pillowblock 1 lOa and an upper pillowblock 1 lOb) fixable to the bedplate 35 of the wind turbine 10 by pillowblock bolts (not shown).
  • pillowblock bolts (not shown).
  • four pillowblock bolts are used to fix the pillowblock 110 to the bedplate 35.
  • the illustrated split pillowblock and bearing assembly 100 includes an inner race ring assembly 115 coupled to a bearing seat 116 (Figs. 4 and 5) of the mainshaft 25 for rotational movement with the mainshaft 25.
  • the bearing seat 116 of the mainshaft 25 is the surface area of the mainshaft 25 that directly contacts the inner race ring assembly 115.
  • the split pillowblock and bearing assembly 100 also includes an outer race ring assembly 120 (Fig. 3) fixed to the pillowblock 110 and positioned between the lower and upper pillowblocks 1 lOa, 1 lOb and the inner race ring assembly 115.
  • the inner race ring assembly 115 defines a two-piece inner race ring having first and second inner ring halves 125, 130 that are connected together about the mainshaft 25 using bolts (not shown). Each inner ring half 125, 130 spans about 180 degrees in arc length and includes two inner raceways 135, 140 (see Fig. 4) that are separated by a central rib 145. First and second series of rolling elements 150, 155 (e.g., tapered rollers) are positioned within a corresponding inner raceway 135, 140. This configuration is often referred to as a “tapered double inner” or TDI race.
  • the central rib 145 is sized and configured to guide and separate the series of rolling elements 150, 155 about the bearing central axis 105.
  • first series of rolling elements 150 are positioned or spaced about the inner ring halves 125, 130, and therefore about the bearing central axis 105, by a first two-piece cage 156.
  • the second series of rolling elements 155 are also positioned or spaced about the inner ring halves 125, 130, and therefore about the bearing central axis 105, by a second two-piece cage 158.
  • the two pieces of each cage 156, 158 are rigidly jointed together by fasteners 159.
  • cage links 162 (Fig. 3) span between the two pieces of each cage 156, 158 for the fasteners 159 to rigidly couple the two pieces of each cage 156, 158 together.
  • roller retainers may temporarily hold the rolling elements 150, 155 within the corresponding cage 156, 158 during assembly of the split pillowblock and bearing assembly 100, as described in detail below.
  • the inner race ring assembly 115 may have more than two halves or portions (e.g., the inner race ring assembly 115 may include three portions spanning about 120 degrees in arc length).
  • the illustrated inner race ring assembly 115 is further coupled to the mainshaft 25 by clamping rings or bands 170 including first and second band halves 175, 180 coupled together by clamping band bolts (not shown).
  • the illustrated clamping bands 170 are sized and configured to fix the inner ring halves 125, 130 relative to the mainshaft 25 to inhibit precession of the inner ring halves 125, 130 and the mainshaft 25.
  • the clamping bands 170 provide an anti-precession mechanism to inhibit relative movement between the inner race ring assembly 115 and the mainshaft 25.
  • Each of the first and second band halves 175, 180 are received within grooves or recesses 185 of the inner ring halves 125, 130.
  • each inner raceway 135, 140 is positioned between the central rib 145 and one clamping band 170.
  • the illustrated first and second band halves 175, 180 span less than 180 degrees in arc length such that split regions or gaps are provided between the first and second band halves 175, 180 when the first and second band halves 175, 180 are coupled to the inner race ring assembly 115.
  • the split regions are circumferentially offset from the split lines of the inner ring halves 125, 130.
  • the clamping bands 170 may have more than two halves or portions (e.g., the clamping bands 170 may include three portions spanning less than 120 degrees in arc length).
  • the portions of the clamping bands 170 may abut (e.g., the first and second band halves 175, 180 span about 180 degrees in arc length to omit the gaps).
  • the illustrated outer race ring assembly 120 includes a first two-piece outer race ring 195, having a first upper half 200 and a second lower half 205, separated from a second two-piece outer race ring 210, having a first upper half 215 and a second lower half 220, by a two-piece outer race spacer 225.
  • the illustrated first two-piece outer race ring 195 also includes a first outer raceway 230 that aligns with the first inner raceway 135 of the inner race ring assembly 115
  • the illustrated second two- piece outer race ring 210 also includes a second outer raceway 235 that aligns with the second inner raceway 140 of the inner race ring assembly 115.
  • the first series of rolling elements 150 are engageable between the first inner and outer raceways 135, 230
  • the second series of rolling elements 155 are engageable between the second inner and outer raceways 140, 235.
  • the illustrated first two-piece outer race ring 195 abuts a shoulder 240 of the upper and lower pillowblocks 1 lOa, 1 lOb to axially position the outer race ring 195 within the pillowblocks 1 lOa, 1 lOb.
  • the spacer 225 abuts the first two-piece outer race ring 195 and the second two-piece outer race ring 210 abuts the spacer 225 opposite to the first two-piece outer race ring 195.
  • the split pillowblock and bearing assembly 100 also includes a two-piece clamping plate 260 coupled to the pillowblocks 1 lOa, 1 lOb via a plurality of adjustable clamping members 265 (e.g., bolts).
  • the clamping plate 260 axially retains the first two-piece outer race ring 195, the second two-piece outer race ring 210, and the spacer 225 between the shoulder 240 of the pillowblocks l lOa, 11 Ob and an axially inner surface 268 of the clamping plate 260.
  • the clamping plate 260 and adjustable clamping members 265 also operate to preload the bearing assembly 100 to improve the life of the split pillowblock and bearing assembly 100.
  • the axial position of the first and second outer race rings 195, 210 can be adjusted relative to the inner raceways 135, 140, thereby changing the preload on the rollers 150, 155, and hence the preload of bearing assembly 100.
  • the split pillowblock and bearing assembly 100 also includes sealing
  • first and second split seal carriers 270, 275 each include a groove that retains a respective split seal member 280, 285.
  • the seal members 280, 285 sealingly engage and run on the outer diameter surfaces of respective split seal wear rings 290, 295, which are coupled to the clamping bands 170.
  • the first seal carrier 270 is secured to an axial end face 300 of the pillowblock 1 lOa, 1 lOb via seal carrier fasteners 305 received in threaded bores 310 formed in the axial end face 300.
  • the second seal carrier 275 is secured to an axial end face 315 of the split clamping plate 260 via seal carrier fasteners 320 received in threaded bores 325 formed in the axial end face 315.
  • a method of replacing an existing pillowblock and bearing assembly (e.g., the pillowblock 30 and the two-row spherical roller bearing 32) on the mainshaft 25 with the illustrated split pillowblock and bearing assembly 100 is described in detail below.
  • the method includes supporting and bracing the mainshaft 25 with, for example, hydraulic jack stands in preparation to remove the existing pillowblock and bearing assembly 30, 32 from the bedplate 35.
  • the existing pillowblock and bearing assembly 30, 32 is unsecured from the bedplate 35 by removing bolts that couple the existing pillowblock and bearing assembly 30, 32 to the bedplate 35 (similar to the pillowblock bolts 112).
  • the existing pillowblock and bearing assembly 30, 32 is then cut off (e.g., by using a gas-flamed torch, grinder, etc.) the mainshaft 25 to remove the existing pillowblock and bearing assembly 30, 32 from the mainshaft 25.
  • the bearing seat 116 is reconditioned and a diameter of the mainshaft 25 is measured to ensure proper fit and clearance between the split pillowblock and bearing assembly 100 and the mainshaft 25 (e.g., optimize an amount of internal clearance built into the split pillowblock and bearing assembly 100).
  • the illustrated split pillowblock and bearing assembly 100 can then be installed onto the mainshaft 25.
  • first and second inner ring halves 125, 130 of the two-piece inner race ring assembly 115 are connected together around the mainshaft 25 by the inner race bolts, and the two-piece clamping bands 170 are clamped over the first and second inner ring halves 125, 130 by the clamping band bolts to further secure the first and second inner ring halves 125, 130 on the mainshaft 25.
  • the illustrated clamping bands 170 are also tightened around the first and second inner ring halves 125, 130 to aid in alignment of the first and second inner ring halves 125, 130 axially along the bearing central axis 105 (e.g., the clamping bands 170 aid in alignment of the inner raceways 135, 140). Furthermore, the clamping bands 170 provide a mechanical anti-rotating feature (i.e., the anti-precession mechanism 184) of the two-piece inner race ring assembly 115 relative to the mainshaft 25. For example, the clamping bands 170 can be tightened as much as possible to establish the gripping force that is needed to prevent precessing of the inner race ring assembly 115 on the mainshaft 25.
  • the method of installing the illustrated split pillowblock and bearing assembly 100 further includes coupling the outer race ring assembly 120, which is affixed to the pillowblock 110, to the inner race ring assembly 115 with the first and second series of rolling elements 150, 155 positioned therebetween.
  • the first and second two- piece retainers 156, 158 are coupled about the inner race ring assembly 115 before the mainshaft 25 can be lowered into the lower pillowblock 1 lOa.
  • the lower pillowblock 1 lOa, the corresponding portion of the outer race ring assembly 120 e.g., the second lower halves 205, 220 and one-piece of the two-piece outer race spacer 225
  • the mainshaft 25 can be lowered into the lower pillowblock 1 lOa by the jack stand for the first and second series of rolling elements 150, 155 to engage the raceways 135, 140, 230, 235.
  • the upper pillowblock 1 lOb, the corresponding portion of the outer race ring assembly 120 (e.g., the first upper halves 200, 215 and the other piece of the outer race spacer 225), and clamping plate 260 are coupled together and positioned over the lower pillowblock 1 lOa and the mainshaft 25.
  • the pillowblock bolts then secure the lower and upper pillowblock 1 lOa, 110b to the bedplate 35.
  • the assembly tool 104 is used to properly position the rollers 150, 155 relative to the raceways. There is clearance for the rollers 150, 155 on the inner raceways 135, 140 between the central rib 145 and respective outer ribs 335.
  • the assembly tool 104 is used.
  • Fig. 5 illustrates a first embodiment of the assembly tool or roller seating device 104 coupled to the bearing assembly 100 just prior to the preloading operation.
  • two assembly tools 104 are shown in use, one at each axial end of the bearing assembly 100.
  • the illustrated assembly tools 104 are identical to one another, so only one will be described below.
  • the tools 104 are split into upper and lower halves (only the upper half is shown in Fig. 5), each extending about 180 degrees. In other embodiments, the tool 104 could have components split into three 120 degree segments, or various other angular split configurations.
  • the tool 104 includes a roller seating actuator 400 removably coupled to a portion of the bearing assembly 100 during the assembly and installation procedure. As shown in Fig. 5, the tool 104 at the right axial end is coupled directly to the clamping plate 260, while the tool 104 at the left axial end is coupled directly to the pillow block housing 1 lOb.
  • the illustrated roller seating actuator 400 has an L-shaped cross-section with an outer leg 405 that abuts an axial end face of the bearing assembly (e.g., the pillow block housing 110b or the clamping plate 260) and an inner leg 410 that extends radially inwardly from the outer leg 405.
  • a plurality of threaded mounting fasteners 415 extend through respective apertures 417 in the inner leg 410 and are positioned to be threadedly engaged with the threaded bores 310, 325 to releasably and temporarily secure the tool 104 to the bearing assembly 100.
  • the same bores 310 and 325 can be used both for initially mounting the tools 104, and for subsequently mounting the seal carriers 270, 275.
  • the tools 104 can be mounted to the bearing assembly 100 in other manners, perhaps using different and dedicated bores formed in various bearing assembly components.
  • the roller seating actuator 400 can be made of steel, other metals, or other rigid materials.
  • the tool 104 further includes a roller seating ring 420 movably coupled to the roller seating actuator 400.
  • the roller seating ring 420 includes a rim portion 425 sized and configured to be positioned adjacent an axial end face of the bearing assembly 100.
  • the rim portion 425 includes a plurality of apertures 430 through which a respective threaded fastener 415 extends with a clearance fit relation.
  • the roller seating ring 420 is in part movably coupled to the roller seating actuator 400 by virtue of the threaded fasteners 415 extending through the apertures 430.
  • the roller seating ring 420 further includes an axially-extending lip portion 435 sized and configured to extend axially from the rim portion 425 into the bearing assembly 100 such that a distal end 440 of the lip portion 435 abuts axial end surfaces 445 of one of the rows of rollers 150, 155.
  • the lip portion 435 of the roller seating ring includes a first portion 450 and a second portion 455.
  • the first portion 450 has a first outer diameter Dl.
  • the second portion 455 includes the distal end 440, is axially-spaced inwardly from the second portion 455 toward the center of the bearing assembly 100 and away from the rim portion 425, and has a second outer diameter D2 that is smaller than the first outer diameter Dl.
  • the first and second portions 450, 455 defined a step in the lip portion 435 that is configured based on the internal components of the bearing assembly 100 to enable the distal end 440 to extend axially into the bearing assembly 100 and engage axially outer end surfaces 445 of the rollers 150 or 155.
  • the specific configuration of the lip portion 435 can be varied as desired depending upon the geometry of the bearing assembly 100.
  • the roller seating ring 420 can be made of a low friction material (e.g., Nylon 66) such that its engagement with the rollers 150, 155 and/or other bearing components will not scratch or otherwise damage those components at the points of contact.
  • the tool 104 further includes a biasing member 460 positioned between the roller seating actuator 400 and the roller seating ring 420 to bias the roller seating ring 420 away from roller seating actuator 400 (i.e., toward the rollers 150, 155). This enables the distal end 440 of the roller seating ring 420 to engage and press the end surfaces 445 of the rollers 150, 155 in an axial direction into engagement with the central rib 145, yet provides a“floating” relationship between the roller seating ring 420 and the roller seating actuator 400 to introduce play and flexibility into the tool 104.
  • the biasing member 460 includes a coil spring placed over at least one of the mounting fasteners 415 and that engages the roller seating actuator 400 at a first end of the spring 460 and engages the roller seating ring 420 at a second end of the spring 460.
  • a spring 460 could be placed over every mounting fastener 415, or less than all of the mounting fasteners 415.
  • other types of biasing members could be used and configured to bias the roller seating actuator 400 and the roller seating ring 420 apart such that the distal end 440 provides the desired force needed to press the roller 150, 155 against the central rib 145, and to also provide the desired play and flexibility.
  • the biasing member 460 (in the form of the coil springs or other members) can be selected to provide the appropriate predetermined amount of force on the rollers 150, 155.
  • the force should be large enough to press or seat the rollers 150, 155 into abutment with the central rib 145, but should not be so large that the friction created between the rollers 150, 155 and the central rib 145 significantly inhibits oscillation of the rollers 150, 155 during assembly and preloading.
  • roller seating actuator 400 and roller seating ring 420 spaced axially apart by a fixed distance (e.g., by the mounting fasteners 415).
  • the installation of the roller seating actuator 400 to the bearing assembly 100 via the mounting fasteners 415 could create the desired force to press the rollers 150, 155 into position against the central rib 145.
  • the roller seating actuator and the roller seating ring could be integrated into a single part.
  • the illustrated mounting fasteners 415 can be threaded along their entire length provided that the apertures 430 in the rim portion 425 provide sufficient clearance from the threads and that the coil spring 460 has a large enough inner diameter so as not to get caught or hung up on the threads.
  • the mounting fasteners 415 can be threaded only at their distal ends to engage the threaded bores 310, 325, and can be smooth and un-threaded over the remaining portion of the shaft.
  • the axial length of the outer leg 405 can be selected so that with the mounting fasteners 415 tightened down completely, the inner leg 410 is spaced the correct axial distance from the axial end surfaces 445 of the rollers 150, 155.
  • the roller seating ring 420 will be adequately spaced axially relative to the roller seating actuator 400 to ensure that the distal end 440 engages the axial end surfaces 445 of the rollers 150, 155 with the desired force to have the rollers 150, 155 properly seat against and abut the central rib 145.
  • the adjustable clamping members 265 and the lower and upper pillowblocks 1 lOa, 1 lOb are tightened to preload the split pillowblock and bearing assembly 100.
  • the outer rings 195, 201 will be forced axially and radially together to increase the preload of the bearing assembly 100.
  • the rollers 150, 155 are secured in position and orientation between the raceways 135, 140, 230, 235.
  • the assembly tools 104 can then be removed.
  • Removal of the tool 104 is achieved by simply removing the mounting fasteners 415 from the respective bores 310, 325.
  • the seal wear rings 290, 295 can be installed onto the clamping bands 170, the seal members 280, 285 are installed into the split seal carriers 270, 275, and the split seal carriers are installed onto the respective pillowblock housing l lOa, 110b and clamping plate 260 via the seal carrier fasteners 305, 320 being installed into the respective threaded bores 310, 325.
  • Figs. 6-10 illustrate a second embodiment of the assembly tool or roller seating device 104’.
  • the assembly tool 104’ differs in several respects from the assembly tool 104, but still operates to achieve the same function of having the distal end 440’ of the roller seating ring 420’ engaging and pressing the end surfaces 445 of the rollers 150, 155 in an axial direction into engagement with the central rib 145.
  • the roller seating actuator 400’ is generally disc-shaped with no axially -extending arm to engage the axial end surface of the bearing assembly 100.
  • the mounting fasteners 415’ still pass though apertures 417’ in the roller seating actuator 400’ and through apertures 430’ in the roller seating ring 420’, and are still threadedly engaged in the threaded bores 310, 325.
  • the assembly tool 104’ further includes additional pins or studs 500 distinct from the mounting fasteners 415’ for interconnecting the roller seating actuator 400’ and the roller seating ring 420’, and for supporting the biasing member(s) 460.
  • the studs 500 each include a head 505 and a distal end 510 spaced from the head 505.
  • the distal ends 510 are secured into apertures 511 in the rim portion 425’ of the roller seating ring 420’ (e.g., by threaded engagement, weld, press fit, adhesive, or other suitable connection methods).
  • the studs 500 are both threaded and secured with adhesive into the apertures 511 in the roller seating ring 420’.
  • the studs 500 pass through apertures 512 in the roller seating actuator 400’ and the head 505 constrains the roller seating actuator 400’ axially on the studs 500.
  • Washers 515 can also be positioned between the heads 505 and the roller seating actuator 400’. This arrangement makes the tool 104’ a more unitized device than the tool 104.
  • a biasing member 460’ (e.g., a coil spring) is positioned over some or all of the studs 500, engages the roller seating actuator 400’ at a first end of the spring 460’, and engages the roller seating ring 420’ at a second end of the spring 460’.
  • the biasing member(s) 460’ bias the roller seating actuator 400’ and the roller seating ring 420’ axially apart.
  • FIG. 9 illustrates one exemplary hole pattern in the roller seating actuator 400’ for the apertures 417’ and the apertures 512 (and therefore also for the apertures 430’ and 511 in the roller seating ring 420’).
  • the hole patterns can vary depending upon the bearing assembly 100.
  • the tool 104’ can take the form of two separate segments of approximately 180 degrees each. Alternatively, the tool 104’ could have components split into three 120 degree segments, or various other angular split configurations.
  • the roller seating actuator 400’ can again be made of steel or other suitable metals or rigid materials, while the roller seating ring 420’can be made of a low friction material (e.g., Nylon 66).
  • the tool 104’ is used in the same manner and with the same methodology as that described above with respect to the tool 104 to properly position and orient the rollers 150, 155 during the preloading operation.
  • the studs 500 and/or the mounting fasteners 415’ could fixedly offset the roller seating actuator 400’ and the roller seating ring 420’.
  • the roller seating actuator and the roller seating ring could be integrated into a single part.
  • the embodiment with the biasing member 460’ and the associated axial displacement facilitates usage and operation of the tool 104’.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Rolling Contact Bearings (AREA)
  • Support Of The Bearing (AREA)

Abstract

Selon l'invention, un outil d'assemblage (104) pour positionner les éléments de roulement (150, 155) d'un ensemble roulement (100) pendant une opération de précharge comprend un actionneur de logement de rouleau (400) configuré de façon à être couplé de manière amovible à une partie de l'ensemble roulement pendant l'opération de précharge, et une bague de logement de rouleau (420) couplée de façon mobile à l'actionneur de logement de rouleau. La bague de logement de rouleau comprend une extrémité distale (440) configurée de façon à venir en prise avec une extrémité d'un élément de roulement de l'ensemble roulement. Un élément de sollicitation (460) est positionné entre l'actionneur de logement de rouleau et la bague de logement de rouleau, et sollicite la bague de logement de rouleau de façon à l'éloigner à partir de l'actionneur de logement de rouleau, de telle sorte que l'extrémité distale de la bague de logement de rouleau vient en prise avec l'élément de roulement et le presse axialement en prise avec une nervure (145) d'un chemin de l'ensemble roulement.
PCT/US2018/055351 2018-02-07 2018-10-11 Dispositif de logement de rouleaux pour roulements à rouleaux coniques WO2019156720A1 (fr)

Priority Applications (4)

Application Number Priority Date Filing Date Title
ES18797280T ES2934069T3 (es) 2018-02-07 2018-10-11 Dispositivo de asiento de rodillos para rodamientos de rodillos cónicos
EP18797280.7A EP3749871B1 (fr) 2018-02-07 2018-10-11 Dispositif de logement de rouleaux pour roulements à rouleaux coniques
US16/967,326 US20200362917A1 (en) 2018-02-07 2018-10-11 Roller seating device for tapered roller bearings
CN201880092082.3A CN111919043B (zh) 2018-02-07 2018-10-11 用于在预负载操作期间定位轴承组件的滚动元件的组装工具和方法

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US201862627348P 2018-02-07 2018-02-07
US62/627,348 2018-02-07

Publications (1)

Publication Number Publication Date
WO2019156720A1 true WO2019156720A1 (fr) 2019-08-15

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PCT/US2018/055351 WO2019156720A1 (fr) 2018-02-07 2018-10-11 Dispositif de logement de rouleaux pour roulements à rouleaux coniques

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US (1) US20200362917A1 (fr)
EP (1) EP3749871B1 (fr)
CN (1) CN111919043B (fr)
ES (1) ES2934069T3 (fr)
WO (1) WO2019156720A1 (fr)

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EP3964725A1 (fr) * 2020-09-02 2022-03-09 Aktiebolaget SKF Procédé d'assemblage d'un roulement et unité de montage correspondant

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DE102020116785A1 (de) * 2020-06-25 2021-12-30 Rolls-Royce Deutschland Ltd & Co Kg Strukturbaugruppe für ein Gasturbinentriebwerk
CN112879443B (zh) * 2021-01-29 2022-03-15 明阳智慧能源集团股份公司 一种兆瓦级半直驱风力发电机组滑环轴承组件的装配工艺
CN113048157B (zh) * 2021-03-12 2022-01-18 深圳市仕瑞达自动化设备有限公司 一种避免钢珠错位的直线轴承装配装置
CN113565867B (zh) * 2021-07-28 2022-03-25 上海交通大学 重力势能发电的轴承滚子自供电监测装置
CN114542609B (zh) * 2022-02-15 2023-02-03 大连理工大学 一种空间轴承预紧力自动控制装置
EP4242483A1 (fr) * 2022-03-07 2023-09-13 Flender GmbH Dispositif palier réglable, en particulier pour éoliennes

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CN111779769B (zh) * 2020-05-18 2022-02-11 上海涟屹轴承科技有限公司 一种新型风电主轴承密封结构
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Also Published As

Publication number Publication date
US20200362917A1 (en) 2020-11-19
EP3749871B1 (fr) 2022-11-30
EP3749871A1 (fr) 2020-12-16
CN111919043A (zh) 2020-11-10
ES2934069T3 (es) 2023-02-16
CN111919043B (zh) 2022-09-20

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